N664WN

Part: LIGHT — LOOSE (CABIN) · airframe 79,409 hrs · 60,820 cycles

DURING SCHEDULED CV CHECK FOUND, LT EEPLS CRACKED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 79,409 hrs · 60,820 cycles

DURING SCHEDULED CV CHECK FOUND, LT EEPLS COVER CRACKED AT ROW 3. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,927 hrs · 60,453 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 316, STR 18R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,924 hrs · 60,453 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 308, STR 18L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,924 hrs · 60,453 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 18R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,924 hrs · 60,453 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 SLAT LOWER T/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 77,481 hrs · 59,348 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE ASSY PER MM AND MT.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 77,184 hrs · 59,123 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT LOWER RADIUS OF DOOR FRAME SKIN CRACKED. REMOVED AND REPLACED R1 DOOR PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 76,505 hrs · 58,600 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 26. REPAIRED BEAM PER ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CHORD CRACKED AT BS 639, RBL 65. REPAIRED CHORD PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 639, WL 213. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 500B TO BS 500C, STR 27L. REMOVED AND REPLACED STRINGER PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED FRAME PER ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 460 TO BS 480, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639, RBL 60. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CRACKED (BS 727B) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 44. REPAIRED BEAM IAW ER AND EA.

Part: WEDGE — CRACKED (LE SLAT) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT WEDGE CRACKED ON LOWER SURFACE. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SKIN — CRACKED (BS 227-235.8) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL POWER DOOR CUTOUT BETWEEN BS 227 TO BS 235.8, BETWEEN STR 19R TO STR 24R. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 44. REPAIRED BEAM PER ER AND EA.

Part: CREASE BEAM — CRACKED (BS 639) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 639, RBL 63. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: FRAME — CRACKED (BS 663 S2-3R) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, BETWEEN STR 2R TO STR 3R. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (BS 639) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 639, LBL 66. REPAIRED FRAME PER ER AND EA.

Part: FLOOR SUPPORT — CRACKED (BS 707-714) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 714, BBL 0. REPAIRED WEB PER ER AND EA.

Part: FLOOR SUPPORT — CRACKED (BS 705-712) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 705 TO BS 712, LBL 24.5. REPAIRED WEB PER ER AND EA.

Part: FLOORBEAM — CRACKED (BS 757B) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 26. REPAIRED BEAM PER ER AND EA.

Part: SKIN — CRACKED (BS 663 S2-3R) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 663, BETWEEN STR 2R TO STR 3R. REPAIRED SKIN PER ER AND EA.

Part: STRINGER — CORRODED (BS 500-500A S26L) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 500 TO BS 500A, STR 26L. REPAIRED STRINGER PER ER AND EA.

Part: FRAME — CRACKED (BS 663 S3L) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (BS 639) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 639, RBL 66. REPAIRED FRAME PER ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 500 TO BS 500A, STR 27L. REPAIRED STRINGER PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787A, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 495, STR 27L. REPAIRED STRINGER PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND L WING O/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,159 hrs · 58,339 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 75,452 hrs · 57,788 cycles

DECLARED EMERGENCY, IN CRUISE NOSE GEAR RED LIGHT ON. WHEN GEAR DOWN NOSE RED UNSAFE LIGHT ON. REMOVED AND REPLACED M1214 & M983 PROX SWITCH RING.

Part: RELAY — FAULTY (NLG) · airframe 75,452 hrs · 57,788 cycles

DECLARED EMERGENCY, ON APPROACH HAD AN UNSAFE GEAR INDICATION NOSE WHEEL RED, NO MAIN LIGHTS. REMOVED AND REPLACED RELAY AND PC CARD.

Part: SENSOR — FAULTY (NLG) · airframe 75,452 hrs · 57,788 cycles

NOSE WHEEL LIGHT RED AT CRUISE ON APPROACH WITH GEAR DOWN NO GREEN LIGHT FOR NOSE WHEEL - GEAR HANDLE TO OFF MANUAL EXTENSION - STILL NO GREEN LIGHT FOR ABOUT A MINUTE. REMOVED AND REPLACED NLG LOCK SENSOR PER MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 75,155 hrs · 57,567 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,425 hrs · 56,999 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EXIT SIDEWALL EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,759 hrs · 56,515 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,759 hrs · 56,515 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 271.5, STR 15L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (LE SLAT) · airframe 73,759 hrs · 56,515 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 4 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,759 hrs · 56,515 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 271.5, STR 15L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,755 hrs · 56,514 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,755 hrs · 56,514 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 COCKPIT WINDOW CUTOUT. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 73,755 hrs · 56,514 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,758 hrs · 56,515 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 271.5, STR 15L. REPAIRED SKIN PER SRM.

Part: TORQUE TUBE — DAMAGED (TE FLAP) · airframe 73,649 hrs · 56,440 cycles

RT WING FLAP SHOWED 30 (LANDING SELECTION) LT WING FLAP SHOWED 25. FOUND TORQUE TUBE DAMAGED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — DAMAGED (TE FLAP) · airframe 73,649 hrs · 56,440 cycles

RT WING FLAP SHOWED 30 (LANDING SELECTION) LT WING FLAP SHOWED 25. FOUND TORQUE TUBE DAMAGED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,457 hrs · 56,308 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,457 hrs · 56,308 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER BULKHEAD ANGLE CORRODED AT BS 727, BETWEEN STR 27L TO STR 27R. REPAIRED ANGLE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,457 hrs · 56,308 cycles

DURING SCHEDULED SPV CHECK, FOUND LT LOWER KEEL BEAM CORRODED AT BS 729. REPAIRED KEEL BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,457 hrs · 56,308 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,019 hrs · 55,954 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270.5, STR 16L. REPAIRED SKIN PER EA.

Part: CONTROL UNIT — FAULTY (AFT CARGO BAY) · airframe 72,347 hrs · 55,469 cycles

DIVERSION, DISCHARGED AFT CARGO FIRE BOTTLE DUE TO FALSE FIRE WARNING INDICATION. FOUND SCU FAILED. REMOVED AND REPLACED SCU PER MM.

Part: HINGE FITTING — BROKEN (SPOILER) · airframe 71,590 hrs · 54,903 cycles

DURING SCHEDULED CV CHECK, FOUND RT WING NR 5 GROUND SPOILER O/B HINGE CASTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 71,590 hrs · 54,903 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 70,736 hrs · 54,304 cycles

FOUND LT EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — MISSING (CABIN) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 EMERGENCY EXIT DOOR LIGHT SIGN MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, FOUND PHOTOLUMINESCENT STRIP CRACKED BETWEEN BS 336 TO BS 947. REPLACED STRIP PER SWA DWG.

Part: SIGN — BROKEN (CABIN) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, R2 EMERGENCY EXIT DOOR SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 14L. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 324 TO BS 340, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 827, LBL 16 TO LBL 18. REPAIRED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER ACO.

Part: SHEAR TIE — CORRODED (BS 360 S27L) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W RT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER ACO.

Part: SKIN — DAMAGED (BS 927 S25R) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S20R) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S22L) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S21R) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 1006 S8L) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S22R) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R AND STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S24L) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CRACKED (LT MLG W/W) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED SPV CHECK, FOUND LT MLG W/W BS 695 FITTING WEB CRACKED. REMOVED AND REPLACED FITTING PER SRM AND BOEING DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,666 hrs · 54,259 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 70,270 hrs · 53,955 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED LENS PER MM.

Part: GLOWSTRIP — WORN (ROW 10 DEF) · airframe 68,768 hrs · 52,833 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 10 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: STRINGER CLIP — CRACKED (BS 727C S7R) · airframe 68,321 hrs · 52,495 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S8R) · airframe 68,321 hrs · 52,495 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S5L) · airframe 68,321 hrs · 52,495 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S6L) · airframe 68,321 hrs · 52,495 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S6R) · airframe 68,321 hrs · 52,495 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,959 hrs · 52,197 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 67,959 hrs · 52,197 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,904 hrs · 51,399 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 66,881 hrs · 51,384 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,570 hrs · 51,142 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,570 hrs · 51,142 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,570 hrs · 51,142 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, LBL 1. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BL 0. REPAIRED SHEAR TIE PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT UPPER FWD CORNER BETWEEN BS 289.5 AND BS 290.5, WL 233 TO WL 255. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 302-304) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 302 TO BS 304, BETWEEN WL 234 TO WL 239. REPAIRED SKIN PER ER.

Part: STRINGER SPLICE — CRACKED (BS 908 S14R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S6L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 727 S23L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 727, STR 23L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727 S23R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 727 S22L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 727, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CORRODED (BS 967 S25L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 25L. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (BS 950 S25L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 950, STR 25L. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (BS 510 S23L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CRACKED AT BS 510. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S14R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 500 S26R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 26R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (BS 502C S25R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CRACKED AT BS 502C. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (BS 727E S14L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 290 S14R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 14R CRACKED AT BS 290. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 867 S14R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 597 S14R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 369 S9L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 369, STR 9L. REPAIRED FRAME PER EA.

Part: STRINGER — CRACKED (BS 706 S9L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 9L CRACKED AT BS 706. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 7L CRACKED AT BS 597. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 440 S9R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S9R) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S9L) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 907, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 440, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 767, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 500C, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 727E, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 400, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 787, STR 9L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 579, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RIGHT WL 201 TO WL 208. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,569 hrs · 51,141 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 65,111 hrs · 50,053 cycles

FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 64,944 hrs · 49,919 cycles

BULL NOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 11 DEF. SECURED LIGHT ASSY PER MM.

Part: CIRCUIT CARD — FAULTY (NLG) · airframe 64,841 hrs · 49,833 cycles

NOSE GEAR SHOWED UNSAFE WHEN LOWERED. RED GEAR LIGHT ON, HORN ON. RECYCLED GEAR WITH NORMAL INDICATIONS. REMOVED AND REPLACED LOGIC BOX AND CIRCUIT CARDS PER MM.

Part: UNKNOWN — UNKNOWN (NLG) · airframe 64,741 hrs · 49,747 cycles

WHEN LOWERING LANDING GEAR, MAIN GEAR INDICATES GREEN, NOSE GEAR INDICATES RED. RECYCLED GEAR HANDLE AND WITH SECOND EXTENSION ALL THREE GEARS INDICATE GREEN. PERFORMED VISUAL INSPECTION OF LOCK SENSORS AND DOWN SENSOR. RERACKED M983 AND M1214 CARDS, OPS TEST OF LOCK SENSORS PER MM.

Part: SKIN — CRACKED (BS 727D S24L) · airframe 64,600 hrs · 49,649 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,226 hrs · 49,361 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 24L. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 64,226 hrs · 49,361 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT INBOARD PULLEY BRACKET BOLT HOLE. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 64,226 hrs · 49,361 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT PER MM.

Part: FITTING — CRACKED (NLG WW) · airframe 64,116 hrs · 49,290 cycles

DURING SCHEDULED A1 CHECK, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSETT CRACKED. REMOVED AND REPLACED NLG GUSSETT FITTING PER SRM.

Part: KEELBEAM — CRACKED (BS 540) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM CRACKED AT BS 540. REPAIRED KEEL BEAM PER SRM.

Part: DOUBLER — CRACKED (BS 517D) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN INTERNAL DOUBLER CRACKED AT BS 517D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: DOOR FRAME — CRACKED (FWD CARGO BAY) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500D) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 21R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 500B) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 21L. REPAIRED FRAME PER SWA EA.

Part: STIFFENER — CORRODED (BS 1016) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 PRESS BULKHEAD LT SIDE RADIAL STIFFENERS CORRODED. REPAIRED STIFFENERS PER SWA EA & BAC DRAWING.

Part: STIFFENER — CORRODED (BS 1016) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 PRESS BULKHEAD RT SIDE RADIAL STIFFENER CORRODED. REPAIRED STIFFENER PER BAC DRAWING.

Part: SKIN — CRACKED (BS 739) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 18L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 927) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: KEELBEAM — CORRODED (BS 500C) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 500C, STR 28L. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (BS 750) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 760) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 947) · airframe 63,559 hrs · 48,864 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 727E) · airframe 63,557 hrs · 48,863 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (R1 DOOR SLIDE) · airframe 63,232 hrs · 48,607 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — CRACKED (BS 768) · airframe 63,232 hrs · 48,607 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 768, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 740D) · airframe 62,912 hrs · 48,360 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 21L. REPAIRED SKIN PER SWA EA.

Part: MODULE — FAULTY (HYD SYSTEM) · airframe 62,884 hrs · 48,340 cycles

AIR TURNBACK, LOST A-SYSTEM HYDRAULIC QUANTITY, HYDRAULIC ENGINE & ELECT PUMPS. REMOVED AND REPLACED HYDRAULIC TAIL ISOLATION VALVE MODULE PER MM.

Part: RELAY — FAULTY (NLG WW) · airframe 62,453 hrs · 48,012 cycles

NLG RED LIGHT ILLUMINATED WITH GEAR HANDLE IN DOWN POSITION. RECYCLED GEAR HANDLE, RED LIGHT EXTINGUISHED. REMOVED AND REPLACED R375 NLG LATCHING RELAY PER MM.

Part: SKIN — CRACKED (BS 500D) · airframe 62,437 hrs · 47,997 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 749) · airframe 62,437 hrs · 47,997 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 61,843 hrs · 47,510 cycles

EMERGENCY LIGHT LENS LOOSE AT ROW 12 DEF. SECURED LENS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,603 hrs · 47,317 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT FUSELAGE EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,375 hrs · 47,142 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,375 hrs · 47,142 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,375 hrs · 47,142 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,375 hrs · 47,142 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,904 hrs · 46,748 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 14.25, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,904 hrs · 46,748 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STR 25R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,904 hrs · 46,748 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 928, STR 25R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,904 hrs · 46,748 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 - 2, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,198 hrs · 46,200 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,796 hrs · 45,877 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 59,415 hrs · 45,592 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT FLAP PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 59,025 hrs · 45,293 cycles

DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 58,576 hrs · 44,920 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR CUTOUT LOWER HINGE BRACKET CRACKED. REPAIRED LOWER BRACKET PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,576 hrs · 44,920 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,576 hrs · 44,920 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,576 hrs · 44,920 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 58,576 hrs · 44,920 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR CUTOUT UPPER HINGE BRACKET CRACKED. REPAIRED UPPER BRACKET PER EA.

Part: LENS — MISSING (CABIN) · airframe 58,568 hrs · 44,917 cycles

DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 4 DEF, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,566 hrs · 44,109 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 57,194 hrs · 43,827 cycles

DURING SCHEDULED, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,634 hrs · 43,373 cycles

DURING SCHEDULED C3 CHECK, FOUND FORWARD EMERGENCY EXIT LIGHT FIXTURE LOOSE. SECURED LIGHT FIXTURE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,393 hrs · 43,172 cycles

PASSENGER CABIN BULLNOSE EMERGENCY LIGHT LOOSE AT ROW 13 ABC. SECURED LIGHT ASSEMBLY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,753 hrs · 42,655 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 727E, STR 20L AND BS 727E+13, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,753 hrs · 42,655 cycles

DURING SCHEDULED C2 CHECK, FOUND 1.25 LONG FUSELAGE SKIN CRACK AT BS 475, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,753 hrs · 42,655 cycles

DURING SCHEDULED C2 CHECK, FOUND .5 LONG FUSELAGE SKIN CRACK AT R2 DOOR UPPER FWD HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 20L. REPAIRED SKIN PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360. STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (CABIN) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CORRODED AT BS 859. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR HINGE CUTOUT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 727D + 10 AND BS 887 + 4, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 440 AT STR 7R, BS 500C AT STR 3R, BS 500C AT STR 2R AND BS 520 AT STR 16C. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND BOTH LEFT AND RT FUSELAGE FRAMES CRACKED AT BS 188, STR 17R AND STR 17L. REMOVED AND REPLACED FRAMES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND 4 EA STRINGER CLIPS CRACKED, BS 500D, STRINGERS 8R AND 7R, BS 500C, STRINGERS 8R AND 7R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CREASE BEAM — CRACKED (FUSLEAGE) · airframe 55,363 hrs · 42,346 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 639 RT SIDE. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,806 hrs · 41,883 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,806 hrs · 41,883 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, BELOW STR 22L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 54,806 hrs · 41,883 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,556 hrs · 41,695 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 213 AND RBL 6.5. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,872 hrs · 41,181 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,214 hrs · 40,663 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT AFT BULB INOP. RELAMPED EXIT LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,956 hrs · 40,464 cycles

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,060 hrs · 39,731 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 4, STR 20L. REPAIRED SKIN PER SRM.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 51,659 hrs · 39,393 cycles

DECLARED EMERGENCY, DURING DESCENT T/E FLAPS WOULD NOT LOWER BELOW 15 DEGREES. REMOVED AND REPLACED T/E FLAP POSITION IND PER MM.

Part: TRU — MALFUNCTIONED (COCKPIT) · airframe 50,753 hrs · 38,647 cycles

DECLARED EMERGENCY, DIVERSION, NR 2 TRANSFORMER RECTIFIER UNIT CB POPPED, FUMES IN CABIN AND FLT DECK, USED FLT DECK 02. REMOVED AND REPLACED TRANSFORMER RECTIFIER UNIT PER MM.

Part: WHEEL — FAILED (MLG)

MAIN WHEEL ASSEMBLY, THROWN TREAD AND 4 BROKEN TIE BOLTS. THROWN TREAD DUE TO LOW PRESSURE CAUSED BY PACKING EXTRUSION PACKING EXTRUSION CAUSED BY BROKEN TIE BOLTS. BROKEN TIE BOLTS CAUSE IS UNDETERMINED. PENDING ENGINEERING EVALUATION.

Part: TIRE — SEPARATED (LT MLG) · airframe 47,927 hrs · 36,280 cycles

AIR TURNBACK, ENGINE SHUTDOWN and DECLARED EMERGENCY. DURING TAKEOFF, NR 2 MLG TIRE SEPARATED DAMAGING NR 1 ENGINE FAN BLADES AND NOSE COWL ASSY. ALSO DAMAGING LT T/E AFT FLAP LOWER SURFACE, LT INBD GROUND SPOILER, LT MLG DOWNLOCK BUNGEE SPRINGS AND LINK ASSY, LT MLG OUTBOARD PRIORITY VALVE HYD LINE AND LT INBOARD T/E LOWER SHELF PANEL. REMOVED AND REPLACED NR 2 MLG TIRE, WHEEL, BRAKE ASSY. REMOVED AND REPLACED NR 1 ENG AND NOSE COWL ASSY. TEMP REPAIRED OTHER COMPONENTS AND MX FERRY TO DAL FOR DAMAGED COMPONENTS REPLACEMENT. ALL WORK DONE PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 47,540 hrs · 35,929 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. READJUSTED EVAC SLIDE ASSY PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD AFT FLAP DELAMINATED AT INBD END. R&R AFT FLAP PER MM.

Part: STIFFENER — CRACKED (MLG WW) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4 CHECK, FOUND BS 663.5 VERTICAL STIFFENER CRACKED AT RBL 6.15. R&R VERTICAL STIFFENER PER SRM.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 2 ENGINE PYLON FRAME CRACKED AT STA 351.88. R&R FRAME PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED AT OUTBD LOWER END. REPAIRED SKIN PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT FRAME CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (LT FLAP) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING INBD FLAP, OUTBD TRACK, UPPER ACCESS PANEL AFT APERTURE FRAME CRACKED. REPAIRED PER SWA RA.

Part: TAB — DELAMINATED (AILERON) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB INBD T/E DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR AFT LOWER CORNER SKIN CUTOUT CRACKED, 1 IN LENGTH. REPAIRED SKIN AND SKIN DOUBLER PER SWA RA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT LBL 12, WL 234, LBL 13.5, WL 234 & RBL 5, WL 195. REPAIRED BULKHEAD WEB CRACKS PER SRM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4 CHECK, FOUND BS 178 BULKHEAD WEB OIL CANNED AT PREVIOUS REPAIR, WL 190, BL 0. REPAIRED BULKHEAD WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED AT BS 750, RBL 3.0 & BS 767, LBL 7.5. REPAIRED FLOORBEAMS PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,463 hrs · 35,857 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR 26L CLIP CRACKED AT BS 867. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,454 hrs · 35,846 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727E, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 47,119 hrs · 35,552 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: RIB — CRACKED (LT WING) · airframe 47,119 hrs · 35,552 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 1.5 INCH CRACK IN LT WING LOWER RIB CHORD, WBL 135.5, AFT END, STRINGER 3. REPAIRED LOWER CHORD PER SWA RA.

Part: SKIN — DELAMINATED (RT WING LE FLAP) · airframe 46,644 hrs · 35,164 cycles

DURING SCHEDULED C4 CHECK, FOUND 15 X 17 DELAMINATION ON RT WING L/E INBOARDD FORE FLAP. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRUT — LOOSE (LT MLG) · airframe 46,644 hrs · 35,164 cycles

DURING SCHEDULED C4 CHECK, FOUND EXCESSIVE PLAY AT LT LWR MLG SIDE STRUT LWR ATTACH BOLT. REMOVED AND REPLACED UNIVERSAL (P/N 65-46106-8) AND SIDE STRUT ASSY PER MM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 45,827 hrs · 34,502 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED. REMOVED AND REPLACED SIDE CHORD PER ACO 7338-54.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 45,733 hrs · 34,427 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 1 SLAT T/E SKIN CRACKED. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 45,733 hrs · 34,427 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT RT OVERWING EXIT. SECURED LENS PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 45,565 hrs · 34,277 cycles

FWD ENTRY DOOR EVACUATION SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY.

Part: EAU — RESET (COCKPIT)

ABORTED TAKEOFF, NR 2 ENG T/R LIGHT ILLUMINATED AND TAKEOFF WARNING HORN SOUNDED. RESET EAU, OPS CK GOOD PER MM.

Part: DUCT — RUPTURED (NR 1 ENGINE)

NR 1 ENG EGT IND 80 DEGREES HIGHER THAN NR 2 ENG, ALSO SLOW TO ACCELERATE. FOUND 9TH STG DUCT RUPTURED ON ENG. REMOVED AND RELACED 9TH STG DUCT.

Part: PC BOARD — FAILED (E & E BAY)

ON TAKEOFF FROM ABQ, LEFT MAIN GEAR RED LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR 2 TIMES, NO HELP. F/O VISUALLY CHECKED GEAR THRU VIEWING PORT AND GEAR APPEARED UP. CONTINUED TO SLC AND AFTER APPROX 15 MIN RED GEAR LIGHT EXTINGUISHED. REPLACED THE M986 AND M988 CIRCUIT CARDS, OPS GOOD PER M/M.

Part: RADOME — BIRD STRIKE (FWD FUSELAGE)

AFTER TAKEOFF AT 1500 FT, LARGE BIRD HIT RADOME. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RADOME ASSY AS PER MM. C/W BIRD STRIKE INSPECTION COMPLIED WITH PER MM 05-51-37. NO OTHER DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND 3 RED EMERGENCY FLOOR TRACKS LIGHTS INOP. RELAMPED PER BOEING M/M.

Part: STRAP — CORRODED (BS 727D)

DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR BEAM SUPPORT STRAP CORRODED AFT OF BS 727D, RBL 16. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (CARGO DR CUTOUT)

DURING SCHEDULED 1/4 D-CHECK, FOUND WEB AT LOWER AFT CORNER OF FWD CARGO DOOR CUTOUT DAMAGED. REPAIRED PER SWA RA 1-A53-1285.

Part: UPLOCK ACTUATOR — FAILED (RT MLG)

DURING CLIMBOUT, RIGHT MAIN GEAR EXTENDED TO FULL DOWN POSITION. CREW RECYCLED GEAR TO UP POSITION AND GEAR OPERATED NORMALLY FOR REMAINDER OF FLIGHT. AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR UPLOCK ACTUATOR, INSPECTED WALKING BEAM BOLT AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.